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J65 aircraft engine
32.778 in. min, 2.788 in. max lg o/a, threaded stem 0.250-28NF-3; body 2.471 in. lg incl 0.565 in. flange; body dia 0.717 in. nom, flange dia 0.934 in. nom; inside dia 0.630 in. nom; nha valve and filter body assy for main fuel control model TJ-L2
FSC 2915 ⁓ Engine fuel system components, aircraft and missile prime movers
Note-fuel components specially designed for propulsion fuel systems, aircraft and missiles are to be placed in this fsc.
Excluding aircraft fuel tanks (fsc 1560); in-flight refueling system fuel components (fsc 1680). fuel system components not specifically designed for use with aircraft engines or missile prime-movers.
Used on j65 aircraft engine.